Explore Books on
aerodynamic load
1-24 of 96 Books
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
By Thomas A. Byrdsong
A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
By Ming Han Tang
High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
By Robert S. Jankovsky
F-18 High Alpha Research Vehicle surface pressures
F-18 High Alpha Research Vehicle surface pressures
By David F. Fisher
In-flight investigation of shuttle tile pressure orifice installations
In-flight investigation of shuttle tile pressure orifice installations
By Timothy R. Moes
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
By Thomas A Byrdsong
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
By Jacob H. Lichtenstein
A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft
A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft
By Lisa J. Bjarke
Fluctuating loads measured on an over-the-wing supersonic jet model
Fluctuating loads measured on an over-the-wing supersonic jet model
By Conrad M. Willis
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
By Jacob H Lichtenstein
Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing
Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing
By Lawrence C. Montoya
Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
By Kerry L. McLallin
Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9
Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9
By William D. Deveikis
Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output
Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output
By P. F. Webster
Aircraft dynamic loads due to flow separation
Aircraft dynamic loads due to flow separation
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
Measurements of heat transfer, flow, and pressures in a simulated turbine blade internal cooling passage
Measurements of heat transfer, flow, and pressures in a simulated turbine blade internal cooling passage
By Louis M. Russell
Nacelle Aerodynamic and Inertial Loads (NAIL) project
Nacelle Aerodynamic and Inertial Loads (NAIL) project
By
Boundary layer effects on unsteady airloads
Boundary layer effects on unsteady airloads
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Structures and Materials Panel.
Unsteady airloads in separated and transonic flow
Unsteady airloads in separated and transonic flow
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Structures and Materials Panel.
The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory
The calculation of generalised forces on oscillating wings in supersonic flow by lifting surface theory
By G. Z. Harris
Aircraft loading and structural layout
By Denis Howe
Studies on air loads on man
Studies on air loads on man
By John J. Swearingen
A method for the prediction of wing response to nonstationary buffet loads =
A method for the prediction of wing response to nonstationary buffet loads =
By B. H. K. Lee